MIL-I-27674 Revision C:1994
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE MULTIFUNCTION, MINUS 5O DEG TO PLUS 2OO DEG C
|
MIL-I-8580 Revision B:1965
|
INDICATOR, TACHOMETER, HELICOPTER, 0-4000 RPM TYPE MA 1
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MIL-I-7065 Revision A:1976
|
INDICATOR, POSITION, AILERON TRIM TAB
|
MIL-I-38121 Revision C:1989
|
INDICATOR, PRESSURE, EGU-9/A
|
MIL I 25688 : A
|
INDICATOR, ELECTRICAL TACHOMETER ERU-3/A. CRANKSHAFT SPEED 500-4,000 RPM, 3 1/4 INCH SIZE
|
MIL-DTL-27188 Revision C:2006
|
INDICATOR, PRESSURE EGU-2/A, OIL, 0-100 PSI
|
MIL-G-25597 Revision D:1973
|
GYROSCOPE, DISPLACEMENT, ROLL AND PITCH, TYPE MD-1
|
MIL-I-83262-1 Revision A:1987
|
INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-31A/A
|
MIL I 7231 : B
|
INDICATOR, TRUE AIRSPEED, SYNCHRO REPEATER TYPE N 1
|
SAE ARP 843 : 2012
|
CHIP DETECTOR, ELECTRICAL CONNECTION, REMOTE INDICATING
|
MIL-I-27202 Revision A:1980
|
INDICATOR, ELECTRICAL TACHOMETER, 0-110 PERCENT RPM 2-INCH SIZE, INTEGRALLY LIGHTED
|
MIL BULL 343 : A
|
DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF
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MIL-STD-1353 Revision C:2014
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ELECTRICAL CONNECTORS, PLUG-IN SOCKETS AND ASSOCIATED HARDWARE, SELECTION AND USE OF
|
MIL-DTL-27723 Revision F:2013
|
Probe, Total Temperature, Deiceable
|
MIL-DTL-28827-1 Revision C:2011
|
SWITCH, THERMOSTATIC (VOLATILE LIQUID), HERMETIC SEALED, SINGLE POLE DOUBLE THROW (SPDT), MEDIUM RESPONSE TIME
|
MIL-G-83872 Revision A:1977
|
GYROSCOPE, DISPLACEMENT, TYPE SBU-23/A
|
MIL-T-38049 Revision A:1972
|
TRANSMITTER, PRESSURE TRU 60A
|
MIL I 38120 : A (3)
|
INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A
|
MIL G 26611 : D
|
GENERATOR, TACHOMETER GEU-7/A, MINIATURE
|
MIL-I-5133 Revision C:1953
|
INDICATOR, ATTITUDE TYPE J 8
|
MIL I 7077 : B
|
INDICATOR, TEMPERATURE ELECTRICAL RESISTANCE, MULTIFUNCTION -70 DEG TO PLUS 150 DEG. C 2 INCH SIZE
|
MIL I 25689 : A NOTICE 1
|
INDICATOR, ELECTRICAL TACHOMETER
|
MIL-I-25325 Revision A:1961
|
Indicator, Rate of Flow, Fuel, Totalizing, 0-100,000 PPH, Type MA-8
|
MIL T 5350 : E
|
TRANSMITTER, SYNCHRO OPERATED, AIRCRAFT, GENERAL SPECIFICATION FOR
|
MIL-I-25863 Revision D:1990
|
INDICATOR, ELECTRICAL TACHOMETER 0-110 PERCENT RPM, 2-INCH SIZE, INTEGRALLY LIGHTED
|
MIL-I-6533 Revision B:1970
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION TYPE G 10
|
MIL I 6839 : C
|
INDICATOR, POSITION, LANDING GEAR
|
MIL-I-5482 Revision C:1960
|
INDICATOR, PRESSURE, SYNCHRO, AIRCRAFT 165 DEGREE SCALE
|
MIL-DTL-83361 Revision B:2007
|
INDICATOR, PRESSURE, OIL, DUAL, 0-100 PSI, EGU-18/A
|
MIL I 25725 : A
|
INDICATOR, TORQUE PRESSURE, MAGNESYN STYLE, SINGLE CLAMP MOUNTED, 2 IN SIZE, 50-400 PSI TYPE A-8
|
MIL-DTL-38394 Revision E:2009
|
Transmitter, Pressure TRU-81/A, Oil, 0-500 PSI
|
MIL-DTL-5790 Revision H:2008
|
Transmitter, Pressure, Oil, Synchro, 0-200 PSI 320-Degree Movement, 26V, Single Phase, 400 Cycles
|
MIL-P-38027 Revision A:1973
|
PRESSURE INDICATING SYSTEM, HYDRAULIC A/A27 J-1
|
MIL I 8136 : A
|
INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12
|
MIL-PRF-25435 Revision D:2008
|
TRANSMITTERS, PRESSURE, AIRCRAFT, GENERAL SPECIFICATION FOR
|
MIL-D-8181 Revision B:1965
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS GENERAL SPECIFICATION FOR
|
MIL-I-27665 Revision B:1984
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE ABU-1O/A, -50 DEGREES TO +50 DEGREES C
|
SAE AS 8181 : 1997
|
DETECTOR, ICE, AIR INTAKE DUCT, AIRCRAFT ENGINES AND AIRFRAME SYSTEMS, GENERAL SPECIFICATION FOR
|
MIL-I-27247 Revision C:1985
|
INDICATOR, TEMPERATURE, SYNCHRO
|
MIL-I-38391 Base Document:1965
|
INDICATOR, ELECTRICAL TACHOMETER, ERU-12/A 0-350 RPM (ROTOR), 0-7000 RPM (ENGINE)
|
MIL I 7491 : B
|
INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1
|
SAE AS 50151 : 2015
|
CONNECTORS, ELECTRICAL, CIRCULAR THREADED, AN TYPE, GENERAL SPECIFICATION FOR
|
MIL-I-25130 Revision B:1974
|
INDICATOR, PRESSURE, OIL, 0-300PSI, TYPE MO-1
|
MIL-I-25479 Revision A:1987
|
INDICATOR, MACH NUMBER, SENSITIVE, SERVOED, RANGE .5 TO 1.O, TYPE ME-5
|
MIL-I-27552 Revision C:1995
|
INDICATOR, TEMPERATURE, THERMOCOUPLE EHU-15A/A, POTENTIOMETER TYPE, WHITE LIGHTED
|
MIL-I-25482 Revision D:1993
|
INDICATOR, ENGINE TESTING
|
MIL-W-18326 Revision A:1956
|
WELDING OF MAGNESIUM ALLOYS, GAS AND ARC, MANUAL AND MACHINE PROCESSES FOR
|
MIL-I-25859 Revision C:1995
|
INDICATOR, THRUST AEU-2/A, SYNCHRO STYLE, PRESSURE RATIO, 1.2-3.4 UNITS, INTEGRALLY LIGHTED
|
MIL-I-83245 Revision A:1994
|
INDICATOR SET, OIL PRESSURE A/A24J-17
|
MIL-I-27673 Revision C:1993
|
INDICATOR, TRUE AIRSPEED AVU-15/A
|
MIL-I-5914 Revision E:1993
|
INDICATOR, RATE OF FLOW, FUEL TYPE EFU 24/A AND TYPE EFU 25/A
|
MIL-I-7087 Revision A:1968
|
INDICATOR, PRESSURE OIL, 0-200 PSI
|
MIL-T-25485 Revision C:1974
|
TRANSMITTER, THRUST, SINGLE SYNCHRO STYLE, PRESSURE RATIO, TYPE MK-2
|
MIL-I-25941 Revision D:1986
|
INDICATOR, TURN AND SLIP, 2-INCH SIZE, INTEGRALLY LIGHTED
|
MIL-I-7084 Revision A:1988
|
INDICATOR, PRESSURE, HYDRAULIC 0-4,000 PSI
|
MIL-T-7258 Revision B:1985
|
TRANSMITTER, TEMPERATURE ELECTRICAL RESISTANCE TYPE B-4
|
MIL T 25435 : B
|
TRANSMITTER, PRESSURE, AIRCRAFT, VARIABLE RELUCTANCE TYPE, GENERAL SPECIFICATION FOR
|
MIL-DTL-7077 Revision D:2011
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION, -70 DEGREES C TO 150 DEGREES C, 2-INCH SIZE
|
MIL-T-5583 Revision C:1987
|
Transmitter, Position, 28 Volts DC
|
MIL-T-25307 Revision D:1985
|
TRANSMITTER, PRESSURE, HYDRAULIC, TYPE MJ-1
|
MIL-I-25437 Revision B:1984
|
INDICATORS, AIRCRAFT, PRESSURE, VOLTAGE RATIO TYPE, GENERAL SPECIFICATION FOR
|
MIL-I-7075 Revision A:1965
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, MULTIFUNCTION -50 DEGREES TO +50 DEGREES C 2 INCH SIZE
|
MIL-T-8249 Revision B:1979
|
TRANSMITTER, RATE OF FLOW, FUEL, TYPE MB-2
|
MIL-I-27667 Revision C:1990
|
INDICATOR, TEMPERATURE, ELECTRICAL RESISTANCE, EHU-16/A MULTIFUNCTION -70 DEGREES TO +150 DEGREES C
|
MIL I 83361 : (4)
|
INDICATOR, PRESSURE OIL, DUAL EGU-18/A, 0-100 PSI
|